| Код ТН ВЭД | 381603 |
Как аккредитованный завод Prodways Stark 3200 Powder for 3D Printing, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.
| Упаковка | Sealed, moisture-resistant industrial 10 kg foil bag clearly labeled Prodways Stark 3200 Powder for 3D Printing, with safety warnings. |
| Погрузка контейнера (20-футовый контейнер) | Prodways Stark 3200 powder for 3D printing is palletized, shrink-wrapped, and secured in a dry 20-foot FCL container for transport. |
| Доставка | Prodways Stark 3200 Powder for 3D Printing is typically shipped as non-regulated, non-hazardous goods in sealed, moisture-resistant containers. Keep dry and away from heat, sparks, static, and dust clouds. Secure and label containers; verify SDS and local dangerous-goods rules before transport. Use appropriate PPE when handling. |
| Хранение | Store Prodways Stark 3200 Powder in a cool, dry, well-ventilated area away from heat, sparks, flames, direct sunlight, and moisture. Keep the original container tightly closed to prevent dust, contamination, and static buildup. Avoid incompatible materials and dust inhalation. Use appropriate grounding/bonding to control static. Follow the manufacturer’s Safety Data Sheet and local regulations for safe handling and storage. |
| Срок годности | Store unopened in a cool, dry place; typical shelf life is 24 months. Protect from moisture, heat, and direct sunlight. |
In orthotic shell manufacturing, Prodways Stark 3200 Powder is charged into a 30 W CO₂ laser powder bed fusion system at a virgin powder fraction of 45–55 wt%, with recovered powder screened to 106 µm and dried at 80°C for 4 h when ambient relative humidity exceeds 60%. The dry blend includes 0.1–0.2 wt% fumed silica flow aid to stabilize spreading, because electrostatic charge above 3 kV has been observed on production-scale powder handling lines to produce layer thickness deviations of ±15 µm. Compliance is anchored to ISO 10993-5:2009 Clause 5.3 for extractable cytotoxicity and ISO 10993-10:2021 for skin sensitization, with batch release records retained under ISO 13485:2016 Clause 4.2.5. The build is executed at a layer thickness of 100–120 µm, a chamber set point of 95–110°C, and a scan spacing of 0.25 mm, followed by in-bed cooling for 8–10 h to reduce curvature. Post-build operations include bead blasting with 0.2–0.4 mm glass beads at 3 bar and optional heat conditioning at 70°C for 2 h to stabilize Shore A durometer readings; without conditioning, lot-specific hardness can drift by +2–3 Shore A over 14 days due to moisture re-equilibration. Terminal products are custom accommodative insoles, metatarsal pads, and heel cups that require extractable cytotoxicity release for each production lot rather than for each shape.
Fatigue-critical midsole builds with Stark 3200 powder use a 60:40 virgin-to-recovered powder ratio by mass, plus 0.3 wt% carbon black masterbatch only for lot traceability. Production campaigns on continuous powder handling lines have shown that recovered powder above 40 wt% raises part porosity from 0.8% to 1.9% under ISO 1183-1:2019 immersion density, and porosity above 2.0% correlates with premature flex-crack initiation under ISO 17707:2005 at 100,000 flex cycles. Builds are nested with a minimum 0.8 mm clearance between shells, sintered at a chamber set point of 110°C and laser energy density of 0.06 J/mm², then tumbled with ceramic media at 22 rpm for 45 min before acid dyeing at 70°C for 30 min. Terminal outputs include running shoe midsoles, hiking boot heel wedges, and orthotic sandals; each lot is tested for Shore A hardness under ISO 868:2003 within 75–85 Shore A and compression set under ASTM D395-18 at 23°C for 22 h below 25%. Published data for this exact powder configuration is limited at recovered fractions above 50 wt%; pre-serial validation is required if the recycling loop operates without sieving below 106 µm.
Powder flow data for footwear runs are tracked with ASTM D6393-14 Carr index measurements; a Carr index below 18% and bulk density between 0.42 g/cm³ and 0.48 g/cm³ are required before loading. Batch-to-batch variation in Shore A hardness is controlled within ±2 Shore A when moisture content remains below 0.05 wt%, and near-infrared moisture analyzers at the hopper infeed divert non-conforming lots.
Because automotive cabin components require burn-rate classification and hydrocarbon resistance, Stark 3200 powder is screened against ISO 3795:2020 and FMVSS 302 before release to small-batch production. The formulation in this segment is held at a 70:30 virgin-to-recovered powder blend with an external flow aid limited to 0.2 wt% fumed silica; recovered powder exceeding 10% of particles below 100 µm is rejected to avoid melt-pool instability and surface pores visible as gloss variation on 30 W CO₂ laser systems. The chamber is inerted with nitrogen to ≤1.5% oxygen, layer thickness is set at 120 µm, and parts are cooled in the powder cake for 6 h before bead blasting with 0.2–0.4 mm glass beads at 3 bar. Burn-rate specimens are excised from 2.0 mm production-representative sheets and tested according to ISO 3795:2020; recorded burn rates below 100 mm/min on 3.0 mm sections are required for cabin air handling components. Terminal parts include HVAC bellows, wire-harness grommets, and isolation damper pads; parts exposed to engine bay temperatures above 90°C should be limited to short-duration contact because compression set rises above 35% under ISO 815-1:2019 at 100°C.
| Application segment | Standard or regulation | Critical clause or test method | Batch release evidence |
|---|---|---|---|
| Orthotic shell | ISO 10993-5:2009 | Extract preparation per Clause 5.3 | Cytotoxicity assay report |
| Footwear midsole | ISO 17707:2005 | Flex fatigue at 100,000 cycles | Crack length ≤1.0 mm |
| Automotive cabin | FMVSS 302 | Burn rate on 3.0 mm section | Burn rate <100 mm/min |
| Automotive cabin | ISO 3795:2020 | Horizontal burning | Not exceeding 100 mm/min |
| Back protector | EN 1621-2:2014 | Transmitted force attenuation | Temperature-conditioned impact curves |
| Brace liner | ISO 10993-23:2021 | Irritation endpoint | Skin irritation grade |
Impact protector geometry in Stark 3200 powder is generated with gyroid or hexagonal lattice cells of 2.5 mm cell size and 1.0 mm wall thickness; the powder bed is run at 100–115°C chamber set point, 100 µm layer thickness, and 0.05 J/mm² laser energy density. The formulation remains 100 wt% Stark 3200 powder with no rigid filler because mineral or glass fillers above 2.0 wt% have been shown to reduce elongation at break below 300% under ISO 527-2:2012 and to compromise force attenuation in back protector testing under EN 1621-2:2014. Powder refresh fraction is held at 75–80 wt% virgin for certification builds, with recovered powder monitored for electrostatic surface charge because charge values above 2.5 kV can cause lattice wall thickness deviation of ±0.08 mm. Build blocks are cooled in the powder cake for 12 h to prevent internal stress concentration, then bead blasted at 2 bar and visually inspected for lattice node cracking before destructive impact testing at -10°C, 23°C, and 40°C. Terminal products are motorcycle back protector inserts, rib protector overlays, and certified lumbar protectors; published data specific to this exact powder configuration in EN 1621-2:2014 dynamic tests is limited, so pre-serial lots require complete transmitted force curves rather than single-point pass/fail values.
A production-scale bottleneck in impact protector builds is lattice node fracture during post-build bead blasting when the energy density is increased above 0.06 J/mm² to raise throughput; this failure mode appears as microcracks at nodes with wall thickness below 0.9 mm, visible only after 10× optical magnification. Operators on 30 W CO₂ systems therefore lock the scan speed to keep node wall thickness above 1.0 mm and reject any powder lot whose flow function coefficient falls below 4.0 under ASTM D6393-14.
Pre-drying at 80°C for a minimum of 4 h is required when ambient storage exceeds 60% relative humidity because moisture uptake above 0.08 wt% broadens the sintering window and creates surface porosity visible on 30 W CO₂ laser systems as gloss variation. In soft-robotic end-effector manufacturing, Stark 3200 powder is used at a 60:40 virgin-to-recovered ratio by mass, with 0.1 wt% antistatic flow aid added only after the recovered fraction has been sieved through a 106 µm mesh. The powder flow function coefficient measured by ASTM D6393-14 is maintained above 4.0 to ensure layer spreading consistency of ±10 µm on production platforms; low-flow lots below 3.5 have caused powder short-feed and localized porosity in gripper pad contact surfaces. Gripper pads are built at 120 µm layer thickness, 110°C chamber set point, and 0.055 J/mm² laser energy density; after cooling for 5 h, parts are spray-coated with a water-based polyurethane varnish at 20 µm dry film thickness to close surface pores and improve repetitive vacuum-pick resistance. Flexural modulus is tested under ISO 178:2019 and compression set under ISO 815-1:2019 at 23°C for 22 h; values above 30% compression set trigger rejection for suction cup collars. Terminal outputs include adaptive gripper jaws, suction cup collars, and cobot end-effector covers that operate in ambient air from 5°C to 40°C.
Cytotoxicity screening data for this powder are generated from 100 wt% Stark 3200 brackets with color masterbatch addition limited to 0.5 wt%; higher additive loadings have been observed to raise extractable cytotoxic response and require re-screening under ISO 10993-5:2009 Clause 5.3. The build chamber is held at 100°C with a 100 µm layer thickness and 0.25 mm scan spacing; after 10 h in-bed cooling, parts are washed in isopropyl alcohol of 99.8% purity for 10 min, dried in a 50°C convection oven for 2 h, and packaged in sealed polyethylene to prevent re-uptake of moisture above 0.05 wt%. Irritation testing follows ISO 10993-23:2021, and skin sensitization data follow ISO 10993-10:2021; these standards are applied whenever the brace or socket interface contacts broken or intact skin for greater than 30 days. Terminal products are knee brace liners, scoliosis pad covers, and prosthetic socket liner shells produced with the same powder lot traceability as orthotic shell runs. Dimensional checks are performed on the internal contact surface at three defined datum positions, with a tolerance of ±0.3 mm; warpage beyond this window has been traced to non-uniform cooling when parts are removed from the powder cake before 8 h.
The table below consolidates typical process envelope data for the seven application segments; values are production-campaign ranges and require lot-specific verification for safety-critical builds.
| Application segment | Layer thickness | Chamber set point | Virgin powder fraction | Critical rejection criterion |
|---|---|---|---|---|
| Orthotic shell | 100–120 µm | 95–110°C | 45–55 wt% | Cytotoxicity failure under ISO 10993-5:2009 |
| Footwear midsole | 120 µm | 110°C | 60 wt% | Porosity above 2.0% under ISO 1183-1:2019 |
| Automotive cabin | 120 µm | 110°C | 70 wt% | Burn rate >100 mm/min under ISO 3795:2020 |
| Back protector | 100 µm | 100–115°C | 75–80 wt% | Lattice wall thickness below 1.0 mm |
| Soft robotic | 120 µm | 110°C | 60 wt% | Compression set above 30% under ISO 815-1:2019 |
| Brace liner | 100 µm | 100°C | 100 wt% | Irritation grade above 1 under ISO 10993-23:2021 |
| Industrial seal | 100 µm | 110°C | 50 wt% | Volume swell above 5.0% under ISO 1817:2015 |
Fluid resistance tests on Stark 3200 seal geometries are executed according to ISO 1817:2015 using mineral oil and dilute acid immersion for 72 h at 23°C; volume swell above 5.0% is cause for rejection in flange gasket service. The powder blend used for non-safety-critical industrial seals is a 50:50 virgin-to-recovered ratio by mass, with a sieve fraction controlled to 100–150 µm and 0.2 wt% fumed silica flow aid; recovered material with fines below 100 µm exceeding 8.0% is discarded to reduce melt-pool instability. Builds are sintered at 110°C chamber set point, 100 µm layer thickness, and 0.05 J/mm² energy density, then post-annealed at 70°C for 2 h to stabilize compression set below 25% after 24 h at 23°C under ISO 815-1:2019. Sealing faces are face-milled flat to Ra 3.2 µm or better; thicker flanges above 6.0 mm require internal lattice cores with 40% triangular infill density to reduce material consumption without collapsing under 150 N clamping force. Terminal products are pump diaphragms, flange gaskets, and anti-vibration mounts for small-batch industrial equipment where chemical contact is limited to mineral oil and dilute acids in the pH 4–9 range; continuous exposure to strong acids or ketones is outside the material's verified compatibility envelope.
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Within the laser-sintering material range of Prodways, Stark 3200 Powder is supplied as an unfilled polyamide 6-based feedstock for powder-bed fusion equipment capable of maintaining elevated build chamber temperatures. Unlike general-purpose PA12 powders, which are specified for ductility and near-isotropic toughness after sintering, Stark 3200 is positioned for rigidity-dependent components in which low-load heat deflection and bending stiffness are limiting design parameters. The designation 3200 corresponds to a nominal tensile modulus near 3200 MPa on XY-printed specimens, although the realised value depends on build orientation, porosity, moisture state, and powder refresh ratio. The material is therefore not a direct substitute for PA12 in snap-fit or high-impact applications.
Bulk powder characterisation according to laser-diffraction protocols typically places the D50 in the 50–60 µm band, with a span suitable for 100–120 µm layer thickness. The tapped density is reported within 0.42–0.48 g/cm³ after standard handling, while the sintered part density measured under ISO 1183-1:2019 is approximately 1.12–1.14 g/cm³. Remaining porosity in standard builds is typically 2–4% by micrographic assessment; this porosity contributes to the Z-direction mechanical anisotropy described below. The powder does not contain glass fibre, carbon fibre, or mineral fillers, and its property profile derives from polyamide 6 chain architecture rather than additive reinforcement.
In production-scale builds on CO₂ laser platforms with 30–60 W source power, the usable energy density for Stark 3200 is narrow because the gap between melting and recrystallization is approximately 45–50°C. When the build chamber is operated below 185°C, the powder bed remains partially crystalline during scanning; the residual crystalline fraction acts as a shrinkage stress concentrator at the layer boundary and can generate z-axis delamination in stable sections thicker than 10 mm. When the chamber exceeds 200°C, the melt pool remains mobile too long after scanning, causing edge growth and loss of fine feature definition. The recommended bed-temperature band is therefore 190–198°C for most open-parameter machines, with a maximum interlayer thermal gradient of 2–3°C across the active build window.
Energy density, calculated from laser power divided by scan speed and scan spacing, must not be treated as a universal constant on different machines. A 100 µm layer thickness requires an energy density near 0.24 J/mm² on a 30 W system, while the same powder on a 60 W machine may tolerate lower scan speeds but exhibits over-sintering at energy densities above 0.30 J/mm². Laser scan spacing is held between 0.20 mm and 0.25 mm to maintain overlap without re-melting adjacent tracks excessively. Operators can detect energetic over-processing by measuring flat-plate curl: when a 150 mm × 150 mm × 3 mm calibration plate distorts by more than 1.5 mm after cooling, the energy input is excessive for the chamber setpoint.
Because polyamide 6 has a higher melt viscosity and lower melt enthalpy per unit volume than many filled systems, recoating temperatures must be maintained within ±3°C of the target bed setpoint across the entire build surface. Temperature variation greater than 5°C between the centre and edges of the build chamber produces differential shrinkage after part extraction and can reduce flatness in tall housings to 0.8 mm per 100 mm of length. Operators using open-parameter Prodways systems should validate the build chamber thermocouple map with an empty bed before each campaign and delay production until thermal stabilisation has been confirmed for at least 45 minutes after reaching setpoint.
Comparative mechanical data, generated on ISO-standard tensile specimens printed in XY orientation, show why Stark 3200 is positioned above standard unfilled PA12 in stiffness and below PA11 in stretch-dominated applications.
| Property | Stark 3200 | Unfilled PA12 | Unfilled PA11 |
|---|---|---|---|
| Tensile modulus, ISO 527-2 | 3000–3300 MPa | 1450–1700 MPa | 1100–1400 MPa |
| Tensile stress at break, ISO 527-2 | 55–62 MPa | 42–48 MPa | 45–50 MPa |
| Tensile elongation at break, ISO 527-2 | 3.5–5.5% | 12–20% | 35–50% |
| Flexural modulus, ISO 178 | 2800–3100 MPa | 1200–1500 MPa | 900–1200 MPa |
| Heat deflection temperature at 0.45 MPa, ISO 75-2 | 175–190°C | 145–155°C | 145–155°C |
| Heat deflection temperature at 1.8 MPa, ISO 75-2 | 85–100°C | 48–55°C | 45–52°C |
| Density, ISO 1183-1 | 1.12–1.14 g/cm³ | 1.00–1.02 g/cm³ | 1.03–1.05 g/cm³ |
The table summarises class-typical values rather than guaranteed minima; specific values for Stark 3200 can shift with build orientation, powder refresh ratio, and post-build conditioning. The measured tensile modulus in the XY plane is normally higher than in the Z plane by 3–6%, while tensile strength in the Z direction may remain at 80–90% of the XY value. Elongation at break is the most orientation-sensitive property and may fall below 3% in z-axis specimens when layer adhesion is incomplete. The stiffness advantage over PA12 is therefore most reliably observed in XY-printed structural ribs, brackets, and jig plates subjected to bending rather than impact.
Where PA12 parts exhibit excessive deflection under load or unacceptable creep at elevated ambient temperatures, Stark 3200 is evaluated for rigid housings, dimensional gauges, assembly fixtures, and underhood vehicle components. Its higher modulus reduces beam deflection for a given cross-section, permitting thinner walls in lightly loaded parts. In a simply supported beam geometry loaded in bending, a part printed with Stark 3200 at 3200 MPa tensile modulus shows approximately 55% less deflection than a comparable PA12 part at 1450 MPa when all other dimensions and boundary conditions are unchanged. This estimation follows linear elastic assumptions and is not a substitute for part-specific finite element verification.
On an open-parameter laser-sintering platform with a 30 W CO₂ source and 100 µm layer thickness, a build campaign of 45 structural brackets showed less than 0.2 mm XY-plane deviation after chamber temperature stabilisation, while Z-oriented holes required a scaling correction of 0.4% in diameter to compensate for shrinkage differences. This behaviour reflects the anisotropic thermal history of the material rather than machine-specific instability and must be accounted for in tooling and assembly fixtures.
The trade-off appears in snap-fit features and thin-walled clip designs. Elongation at break below 6% means that snap-fit undercuts designed for PA12 at 2–3% strain may operate too close to yield in Stark 3200. Replacement parts require an increase in flexural hinge length or a reduction in engagement depth to keep outer-fibre strain below 2.5% under assembly deflection. For a cantilever snap with rectangular cross-section, the maximum permissible deflection is proportional to beam length squared and thickness; increasing the length by 20% reduces the peak strain by approximately 36% for the same undercut depth. Published data for this specific configuration is limited, so strain should be validated on printed test pieces.
Underhood brackets exposed to radiant heat from exhaust manifolds require heat deflection temperatures above 150°C at 0.45 MPa, which unfilled PA12 cannot provide. However, the material is not a substitute for PA6 with glass fibre or carbon fibre where continuous service above 150°C under load is required; its deflection temperature under 1.8 MPa remains below 100°C. Parts with high impact requirements, particularly at sub-zero temperatures, should be evaluated using instrumented puncture tests because unfilled PA6 can show a ductile-to-brittle transition that is not present to the same degree in PA11.
Polyamide 6 powder is hygroscopic. Stark 3200 exposed to air at 60% relative humidity and 23°C can absorb sufficient moisture within 4 hours to degrade part density and surface quality. Pre-drying at 80–90°C for 8–12 hours in a desiccant or vacuum dryer is required before reintroducing stored powder into production. Conditioned moisture content should be below 0.10% by Karl Fischer titration. Use of powder above 0.15% moisture typically raises melt viscosity and produces orange peel surfaces, pinhole porosity, and an increase in Z-direction strength loss.
Virgin powder must be stored in sealed containers at 15–25°C and below 40% relative humidity. If a container is opened in a high-humidity moulding environment, the powder should be dried before use. Drying at temperatures exceeding 90°C or for longer than 12 hours can cause thermal ageing and shift the melt flow rate beyond the recycled powder specification. Use of vacuum drying at 80°C for 6–8 hours is preferred where available.
Powder refresh is managed to counteract molecular weight increase and yellowing caused by repeated exposure to 185–200°C bed temperatures. Used powder from previous builds is mixed with virgin powder at a ratio of 30–40% fresh stock for dimensional-critical parts; for lightweight non-structural parts, the fresh fraction can be reduced to 20% if the used powder is sieved at 150 µm and its melt flow rate remains within the specification band. The melt volume-flow rate measured at 235°C with 2.16 kg load under ISO 1133-1:2022 is a practical incoming indicator; a drop of more than 35% from the virgin value indicates that the recycled fraction has undergone sufficient chain extension to require a higher virgin ratio.
The powder should not be blended with PA12 or PA11 feedstock because the differing melt temperatures and crystallization rates create localised unfused agglomerates and mechanical weaknesses in the sintered part. Additives containing amine groups can accelerate oxidative discolouration of the polyamide matrix at build temperatures; material compatibility with external flow agents or surface treatments should be confirmed before production. Part acceptance testing for Stark 3200 should include tensile bars built in XY and Z orientation per ISO 527-2, flexural coupons per ISO 178, and density measurements per ISO 1183-1 on each build campaign. Operators commonly monitor part mass and dimensional drift; a build-to-build mass variation of more than 1.5% indicates either powder moisture uptake or insufficient refresh.
From a compliance standpoint, the powder is supplied with safety data sheet and labelling under EU CLP 1272/2008. RoHS 2011/65/EU obligations apply to final electrical and electronic equipment, not to the powder alone. No claim for food contact or medical use should be derived from standard documentation unless specific migration testing under EU 10/2011 or biocompatibility evaluation under ISO 10993 has been completed for the intended article. Unfilled PA6 powders are not inherently flame retardant; UL 94 HB is the default classification, and any V-0 rating requires additive packages not present in this grade. These regulatory limitations should be communicated to downstream manufacturing teams before adopting Stark 3200 into serial production.